Stress-analysis procedure in unsymmetrical loading conditions; unsymmetrical loads on cantilever wing; side-load analysis for engine mount with three points of support; wing-spar analysis; tail-surface analysis based on deflections; landing-gear analysis.
Late developments in airplane stress-analysis methods and their effect on airplane structures
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 31 , n 3
1932
11 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Late Developments in Airplane Stress-Analysis Methods and Their Effect on Airplane Structures
SAE Technical Papers | 1932
|NTRS | 1918
|Engineering Index Backfile | 1920
|SLUB | 1954
|Engineering Index Backfile | 1938